MS-500V
The engines are intended for installation in civil purpose helicopters with takeoff mass of 3.5 to 6 t and permit to attain high economic standards in the course of commercial use. |
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Main advantages of the engine:
- simple and effective design;
- high reliability;
- low specific fuel consumption;
- high stability of characteristics in service;
- compliance with current and future environmental requirements;
- extended service life and durable calendar life;
- ease and convenience of maintenance and repair;
- low cost of life cycle.
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Basic specifications:
| Engine |
MS-500V |
MS-500V-01 |
MS-500V-02 |
| With one engine inoperative (OEI) (SLS, ISA): |
2,5-min power; hp (kW)
(flat-rated to tAMB, °C) |
710 (522)
(+35) |
1000 (735)
(+15) |
1200 (833)
(+20) |
30,0-min power; hp (kW)
(flat-rated to tAMB, °C) |
659 (485)
(+40) |
850 (625)
(+30) |
1000 (735)
(+35) |
| Take-off power rating (SLS, ISA): |
Power, hp (kW)
(flat-rated to tAMB, °C) |
630 (463)
(+35) |
810 (596)
(+35) |
950 (699)
(+35) |
| Cruise power rating (SLS, ISA) |
Power, hp (kW)
(flat-rated to tAMB, °C) |
450(331)
(+50) |
450(331)
(+50) |
500(368)
(+50) |
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